Browse Topic: Hydraulic motors

Items (168)
Internal combustion (IC) engines experience several parasitic losses at the vehicle level, including those from cooling fans, hydraulic pumps, air compressors, and alternators. These losses limit the available output power for various applications. By replacing a conventional mechanical or hydraulic fan—typically driven by the engine crankshaft or hydraulic motor—with an electrically operated fan, engine frictional losses (fan drag) can be reduced, resulting in a gain in power. The fuel conserved due to the absence of fan drag contributes to usable power for applications. Mechanical fans operate at a fixed drive ratio that is directly proportional to engine speed, while hydraulic fans rely on a hydraulic motor, drawing power from the engine's alternator. In contrast, electric fans can run at constant speeds, independent of engine RPM, providing higher airflow at maximum torque speeds, which mechanical fans cannot achieve. The cooling performance of the engine remains uncompromised, as the electric fan can be strategically positioned in the optimal airflow zone through computational fluid dynamics (CFD) analysis. Unlike mechanical fans, which operate in a single direction, both hydraulic and electric fans can rotate clockwise or counterclockwise. Electric fans have the added advantage of functioning with reverse polarity in the electrical circuit. This capability allows them to act as blowers, helping to keep heat exchange cores clear of debris during dusty applications for the construction machines on the site, which can restrict airflow when using a conventional puller-type fan. The replacement of electric fans resulted in a significant power saving which resulted in lesser load on hydraulic oil cooler in the case of hydraulic fan.
Dewangan, NitinKattula, NitinKamal, Ankit
Rolling bearings with optimized friction and performance characteristics can have a significant influence on reducing the power loss, design envelope and weight of hydraulic motors and pumps, gearboxes and axles in construction machinery. If correctly designed, rolling bearings can make a significant contribution to reducing carbon dioxide emissions. Most construction machinery is still operated conventionally, using diesel engines and hydraulic components. In the widely used adjustable axial piston pumps and motors, the input and output shaft are usually supported by two tapered roller bearings that are adjusted against each other. When designing the bearing support, it is advisable to reduce the preload to precisely the required minimum allowed by the load spectrum. The lower bearing preload leads to permanently lower axial forces between the tapered roller end face and inner ring rib and, therefore, to a corresponding reduction in frictional torque.
Scharting, Stefan
This test code describes tests for determining characteristics of hydraulic positive displacement motors as used on off-road self-propelled work machines as referenced in SAE J1116.
CTTC C1, Hydraulic Systems
The techniques outlined in this SAE Recommended Practice were developed as part of an overall program for determining and evaluating fuel consumption of heavy-duty trucks and buses, but it is applicable to off highway vehicles as well. It is recommended that the specific operating conditions be carefully reviewed on the basis of actual installation data. Cooling requirements are affected by all heat exchangers that are cooled by the fan drive system. These may include radiators, condensers, charge air coolers, oil coolers, and others. Because of the variation in size, shape, configuration, and mountings available in cooling fans and fan drive systems, specific test devices have not been included. Using known power/speed relationships for a given fan, this procedure can be used to calculate the fan drive system’s power consumption for cooling systems using the types of drives listed below. This power consumption may then be used in determining engine net power per SAE J1349. For more fan power/speed relationships, refer to SAE J1339.
Cooling Systems Standards Committee
This SAE Aerospace Information Report (AIR) provides descriptions of trimmable horizontal stabilizer actuators that are installed on a variety of transport and business aircraft systems.
A-6B3 Electro-Mechanical Actuation Committee
This SAE Aerospace Recommended Practice (ARP) is an application guide for fixed and variable displacement hydraulic motors. It provides details of the characteristics of fixed and variable displacement hydraulic motors, architectures, circuit designs, controls, and typical applications. The applications include airborne and defense vehicles with emphasis on high performance applications.
A-6C4 Power Sources Committee
This SAE Aerospace Standard (AS) provides a system of graphic symbols and line codings that are intended primarily for usage in hydraulic and pneumatic system schematic diagrams for all types of aircraft.
A-6 Aerospace Actuation, Control and Fluid Power Systems
This Recommended Practice provides a guide for specifying general design, performance, and test requirements for power drive units (PDUs) for flight controls and other applications.
A-6B3 Electro-Mechanical Actuation Committee
This test code describes tests for determining characteristics of hydraulic positive displacement motors as used on off-road self-propelled work machines as referenced in SAE J1116.
CTTC C1, Hydraulic Systems
To describe laboratory methods for determining and reporting the contaminant level of the wetted portion of hydraulic fluid power components, parts, subsystems and systems, and of fill fluids. For each type of item, it provides a method of obtaining the liquid sample and the contamination level thereof. It also includes procedures for establishing a sampling plan and guidelines for establishing levels of acceptance, but does not set those levels.
CTTC C1, Hydraulic Systems
Optimum Sizing of Hydraulic Pump in Vibratory Roller Vehicle Propulsion System2019-26-01051/9/2019
Vibratory roller also known as vibratory compactor is a construction equipment vehicle designed for soil compaction which increases the load bearing capacity of cohesive and granular soils. Primary requirement from the industry is to achieve the highest unit volume compaction with lowest fuel consumption and lesser operating expenses spent by end users. In typical vibratory rollers, hydrostatic drive system is used for vehicle propulsion which comprises of one variable displacement hydraulic pump and two hydraulic motors connected in parallel. Between the two motors, one is a dual displacement motor at rear axle drive and the other is a single displacement motor at front drum drive to achieve two different vehicle speeds in Travel and Work modes. This paper describes the hydraulic system design which differs from conventional system by adapting a dual displacement motor at front drum drive to achieve the desired vehicle speed. This new configuration generates four different vehicle speeds by setting different combination of displacements of the two motors using an electrical actuator valve in a particular sequence of mode. By having the new lowest speed mode, which is selected through a switch by the operator, vehicle can climb the higher gradient of >40% for the given engine power and it has been additionally introduced as “Gradient mode” a new feature apart from regular Travel and Work modes of the vehicle. Benefit from this new system design is the 40% reduction in hydraulic pump displacement size which gives significant cost savings of around 39%, Motor type change from Single displacement to dual displacement and inclusion of actuator valve increases the cost by 5%. Overall, cost savings of around 22% is achieved and additional mode is introduced as a new feature in the vehicle. Also, the reduced pump size helps in reducing hydraulic oil quantity in the system, thereby reducing carbon foot print.
Velusamy, KarthikeyanSundararajan, SureshkumarThukkaiyamoopar Anbarasu, Raja Raja CholanSellamuthu, Myilsamy
SAE J1362 presents graphical symbols for use on operator controls and other displays on off-road work machines as defined in SAE J1116 plus mobile cranes but excluding agricultural tractors. Symbols for agricultural tractors are covered by ASABE S304, ISO 3767-1, and ISO 3767-2.
HFTC2, Machine Displays and Symbols
This Specification covers constant displacement hydraulic motors, generally remotely mounted, using hydraulic fluid under pressure as the energy transfer medium for driving various accessories. Hydraulic motors shall be suitable for use in aircraft hydraulic systems conforming to and as defined in MIL-H-5440 and MIL-H-8891 as applicable.
A-6C4 Power Sources Committee
This SAE Aerospace Information Report (AIR) provides design information of various contemporary aircraft fly-by-wire (FBW) flight control actuation systems that may be useful in the design of future systems for similar applications. It is primarily applicable to manned aircraft. It presents the basic characteristics, hardware descriptions, redundancy concepts, functional schematics, and discussions of the servo controls, failure monitoring, and fault tolerance. All existing FBW actuation systems are not described herein; however, those most representing the latest designs are included. While this AIR is intended as a reference source of information for aircraft actuation system designs, the exclusion or omission of any other appropriate actuation system or subsystem should not limit consideration of their use on future aircraft.
A-6A3 Flight Control and Vehicle Management Systems Cmt
This SAE Standard applies only to new winches which are primarily designed for intermittent pulls and lifts and whose configuration and condition are the same as when they were shipped by the manufacturer. They are not intended to be used in any manner for the movement of personnel. They may be driven by any power source recommended by the manufacturer and will be capable of being powered in either direction. They will be equipped with an automatic safety brake system to control a load when lowering under power and positively hold a load when power is not being delivered to the winch. A hydraulic flow control valve or similar device may be used in the brake system to control a load when lowering under power. A clutch to release the drum for “free-spooling” may be provided and will be designed not to disengage itself under load. A drag brake may be provided to control “free-spooling,” but will not be relied on to control or hold a load. Power sources, such as hydraulic motors, even though they may be supplied or recommended by the winch manufacturer, are not considered a part of the winch so far as this document is concerned, except to whatever extent they are a part of the brake system.
Truck and Bus Powertrain Committee
Three levels of fan structural analysis are included in this practice: a Initial Structural Integrity b In-vehicle Testing c Durability (Laboratory) Test Methods The Initial Structural Integrity section describes analytical and test methods used to predict potential resonance and, therefore, possible fatigue accumulation. The In-vehicle (or machine) section enumerates the general procedure used to conduct a fan strain gage test. Various considerations that may affect the outcome of strain gage data have been described for the user of this procedure to adapt/discard depending on the particular application. The Durability Test Methods section describes the detailed test procedures for a laboratory environment that may be used depending on type of fan, equipment availability, and end objective. The second and third levels build upon information derived from the previous level. Engineering judgment is required as to the applicability of each level to a different vehicle environment or a new fan design. This SAE Recommended Practice is applicable to any engine cooling fan application including medium and heavy-duty trucks, buses, construction equipment, industrial, and agricultural equipment. Some sections are more applicable to engine-driven fans than to hydraulic-driven or electric-motor-driven fans, especially with respect to speed control. Fan failure modes, however, are generally the same regardless of driving modes. The usage of non-metallic construction necessitates areas of evaluation not required by metallic designs. Chief among these are temperature extremes, moisture content, impact resistance, chemical attack, material purity/homogeneity, and aging/weathering. Areas of evaluation affecting both metallic and non-metallic fans, but requiring somewhat different approaches with non-metallic parts, include natural frequency determination and durability testing.
Cooling Systems Standards Committee
This SAE Aerospace Information Report (AIR) presents an overview of the application and control of fixed and variable displacement pumps with the emphasis on the controls most commonly used on variable displacement pumps. It describes various options to control the operation of hydraulic pumps in terms of controlling the pump output pressure and/or flow and assisting in the selection of the pump.
A-6C4 Power Sources Committee
With the ever increasing number of vehicles on road and the rise of the electric and automated vehicles, it is important to minimize the consumption of energy by each vehicle, regenerative braking is in wide use today, however, the research in the field of regenerative suspension is limited. The regenerative suspension has huge capabilities in power generation especially on third world roads having rather bumpy rides. A huge amounts of energy is wasted in shock absorbers due to friction. This study emphasizes on the implementation of the energy present in the suspension system by replacing the Shock Absorber with a Energy transfer system Involving Hydraulic cylinder, Hydraulic Motor and Dynamo. The energy which is usually lost as heat due to friction in conventional Suspension is used to drive a dynamo through Hydraulic System designed in this paper and electricity is generated. This approach involves design and simulation of regenerative suspension system with specialized hydraulic device and comparison of the system with regenerative suspension system involving Rack and Pinion. Electricity is generated by the Regenerative System and plot of the electricity generated with the speed of the vehicle is obtained using simulation. A marked Improvement is seen in the energy saved using this system as compared to simple Suspension system.
Ahmad, KhushalAlam, Monis
This report contains background information on life cycle cost elements and key ECS cost factors. Elements of life cycle costs are defined from initial design phases through operational use. Information on how ECS designs affect overall aircraft cost and information on primary factors affecting ECS costs are discussed. Key steps or efforts for comparing ECS designs on the basis of LCC are outlined. Brief descriptions of two computer programs for estimating LCC of total aircraft programs and their use to estimate ECS LCC, are included.
AC-9 Aircraft Environmental Systems Committee
The cooling system with two fans is generally driven by electrical motors in the small cars. Compared with the traditional cars, heavy duty trucks have the larger heat dissipation power of cooling system. The motors power consumption of dual fans will be larger and the two electrical motors will occupy a large space in the engine cabin. Hydrostatic drive refers to the cooling fan is driven by hydraulic motor, but it has the low transmission efficiency. According to the engine water temperature value and the actual working status of the hydraulic system, the actual speed of cooling fan can be controlled by the computer, which guarantees the normal working water temperature of the engine. Hydrostatic drive is generally applied to heavy vehicles, engineering machinery and excavators as driving source of cooling fan which contains the advantages of large output power, overload protection, continuous speed regulation and flexible space arrangements. Integrating the characteristics of the driving modes with the hydraulic motor and electrical motor, the two motors of cooling fan can adopt cooperative operation using both driving modes. In the situation of low heat dissipation power, the cooling fan only can be driven by electrical motor, and two motors work cooperatively when the engine have the high heat dissipation power. By means of establishing the fuzzy control strategy, the rotary speed of two motors can be adjusted according to the real-time engine water temperature variation. Compared with the conventional PID control, the fuzzy control can avoid overshoot and improve temperature control precision. Owning to the overflow loss of hydraulic valve, the performance analysis of two driving modes with two hydraulic motors and the dual electro-hydraulic motors will have a comparison. The results prove that the power consumption of pure hydraulic system is 5.3kW while the power consumption using dual electro-hydraulic motors is 3.5kW, so that the power consumption saves 34% on average.
Zhang, XingyuYang, BoWang, CanLi, ZhileiGe, YongqiangYang, ZhongjieLiu, Xue
In this paper a new pressure control method of a modified accumulator-type Electro-hydraulic Braking System (EHB) is proposed. The system is composed of a hydraulic motor pump, an accumulator, an integrated master cylinder, a pedal feel simulator, valves and pipelines. Two pressurizing modes are switched between by-motor and by-accumulator to adapt different pressure boost demands. A differentiator filtering raw sensor signal and calculating pedal speed is designed. By using the pedal feel simulator, the relationship between wheel pressures and brake force is decoupled. The relationships among pedal displacement, pedal force and wheel pressure are calibrated by experiments. A model-based PI controller with predictor is designed to lower the influences caused by delay. Moreover, a self-tuning regulator is introduced to deal with the parameter’s time-varying caused by temperature, brake pads wearing and delay variation. To verify the controller validity, a Rapid Control Prototype (RCP) test environment based on dSPACE is built. Self-designed HCU and pedal feel simulator are installed in test bench. The close loop test results of pressure tracking are plotted and analyzed by contrasting normal PI controller and proposed controller. The conclusion indicates that the proposed controller can reach a balance of rapidity and accuracy, meanwhile the operating time and energy consumption are also reduced.
Xiong, ZhePei, XiaofeiGuo, XuexunZhang, Chengcai
The heavy duty trucks have large engine power and drive continuously in mountainous area, so the heat dissipation of engine is very important. In the traditional cooling system with fixed transmission ratio fan, the cooling capacity is insufficient and the engine is easy to be over-heated when the engine is working in low speed and heavy load conditions. Owning to the bigger size of electric motor compared to the hydraulic motor, it is not suitably applied to the heavy duty trucks. Contrasted with the electric motor, the hydraulic drive cooling system is widely applied in heavy duty trucks due to smaller size, larger power, continuous speed modulation and flexible installation location. However, the low transmission efficiency of the pump-motor system results in high power consumption of the cooling system. In this paper, the mathematical and simulation model of hydraulic-driven fan cooling system is established for the specific engine. The study applies the digital PID controller of continuous system to control the fan. The control algorithm of anti-integral saturation is compared with the conventional method. The results show that during the time progress of 700s, the mean power consumption with anti-integral algorithm respectively reduce by an average of 40.8%, 35.1% and 29.2% in the target temperature of 363.15K, 364.15K, and 365.15K compared with the traditional control method. Moreover, the PID control with anti-integral algorithm can improve the temperature control accuracy and effectively avoid the excessive cooling.
Zhang, XingyuYang, BoTan, GangfengMei, BinyuLi, ZhileiYang, ZhongjieWang, Can
This SAE Aerospace Information Report (AIR) applies to landing gear tires and airframe structure for all types and models of civil and military aircraft having tires as part of the landing gear.
A-5C Aircraft Tires Committee
It is important for engineering firms to be able to develop forecasts of recommended courses of action based on available information. In particular, engineering firms must be able to assess the benefit of performing information-gathering actions. For example, an automobile manufacturer may use a computer simulation of a hydraulic motor and pump in the design of a new vehicle. The model may contain random variables that can be more accurately determined through expensive information-gathering actions, e.g., physical experiments, surveys, etc. To decide whether to perform these information-gathering actions, the automobile manufacturer must be able to quantify the expected value to the firm of conducting them. However, the cost of computing the expected value of information (through optimization, Monte Carlo sampling, etc.) grows exponentially with the amount of information that is to be gathered and can often exceed the cost of actually gathering the information. Thus, if information decisions are to be addressed algorithmically, there exists a need for novel algorithmic approaches to reduce the computational expense associated with computing the expected value of gathering information. The contribution of this paper is a novel algorithmic approach for approximating the expected value of perfect information (EVPI) for engineering design problems. In this research, we propose to recast the EVPI as a “parametric” problem. The value of recasting the problem is an exponential reduction in the computational complexity. The proposed approach is validated against a Monte Carlo sampling based approach, the traditional approach for solving EVPIs, on an engineering problem. The engineering problem is to compute the expected value of performing physical experiments to gather information about random variables in a computational model the efficiency of an engine and transmission. The results are compared in terms of computational expense and solution accuracy. The results indicate that by recasting the EVPI as a parametric problem the computational expense is reduced drastically while maintaining solution accuracy.
Galvan, EdgarHsiao, ChuckVermillion, SeanMalak, Richard
Nowadays, off-highway vehicles enjoyed a significant status in the national defense and civil construction. There is no doubt that the working conditions of off-highways are quite different from the conventional passenger cars, hence, their suspensions are particularly designed. Since the hydro-pneumatic suspension technology is maturely applied in engineering machinery, this paper presents a concept for a novel energy-harvesting device, which is applied in off-highway vehicles based on hydro-pneumatic suspension, namely, electro-hydraulic energy-harvesting suspension (EHEHS). The EHEHS took the fundamental of mechanism-electronic-hydraulic system, which consisted the following elements: a cylinder, 2 check valves, a hydro-pneumatic spring, a hydraulic motor, a DC motor, a processing circuit and a battery. In the EHEHS system, the cylinder is used to transmit the vibration energy into hydraulic energy, which is stored in hydro-pneumatic spring. The hydraulic motor is the energy conversion device that could translate the hydraulic energy into rotational kinetic energy, which could be converted into electric energy by the electric motor. The final electric energy is conserved in the battery after treatment by the processing circuit. Apart from the description of the configuration of the EHEHS, this paper also discuss the stiffness and damper characteristic of the novel energy-harvesting suspension by mathematic derivation, and a simulation based evaluation is present to show its application in an off-high way commercial vehicle.
Zhou, QuanGuo, XuexunXu, LinWang, GuolingZhang, Jibing
Nearly 1000 university teams from 55 countries around the globe entered the first Valeo Innovation Challenge, the goal of which was to ‘design the product or system that will make the cars of 2030 smarter and more intuitive.’ THE UNIVERSIDADE FEDERAL DE MINAS GERAIS OF BRAZIL TOOK FIRST PRIZE, and a cash award of €100,000, in the first Valeo Innovation Challenge. Tying for second place and taking home €10,000 each were Canadian teams: the University of Ottawa and the University of Waterloo. The Brazilian team's project aims to reinvent the mechanical transmission system by coupling together the pump and the hydraulic motor. This innovation would enable the transmission to adjust to engine rpm continuously and automatically, thereby improving fuel efficiency and reducing CO2 emissions.
This SAE Aerospace Recommended Practice (ARP) is an application guide for hydraulic power transfer units and describes: The various types Typical design approaches Their operational characteristics and limitations Circuit recommendations Typical applications The scope of this ARP is limited to devices that transfer power between hydraulic systems and do so by means of rotary subassemblies such as hydraulic motors and pumps.
A-6C4 Power Sources Committee
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a commercial transport rotorcraft hydraulic system, including the applicable airworthiness regulations that affect the hydraulic system. This ARP also provides information and guidelines on the many factors that arise in the design process to provide cost effectiveness, reliability, maintainability and accepted design and installation practices.
A-6A1 Commercial Aircraft Committee
Due to the high demand of fuel efficient construction equipment, significant research effort has been dedicated to improving excavator efficiency. Among various possibilities, methods to recuperate energy during cab swing motion have been widely examined. Electric and hydraulic hybrids designs have shown to greatly improve fuel efficiency but require drastic design changes. The redesigned systems thus require many hours of operation to offset the manufacturing costs with fuel savings. In this research, a relatively simple swing energy recuperation system is presented using an additional accumulator, fixed displacement hydraulic motor, and control valves. With the system, hydraulic fluid is stored in an accumulator, and a simple controller opens a valve to allow the stored energy to assist the engine in running the main pumps. Using various accumulator capacity and hydraulic motor displacement combinations, the recuperation system was simulated for six cycles of a digging and dumping operation. The simulation results show that an optimum configuration reduces the swing energy consumption by 48% and the total excavator energy by 17% during digging and dumping operations.
Thompson, BradleyYoon, Hwan-SikKim, JaehongLee, Jae
This SAE Aerospace Information Report (AIR) establishes the specifications and descriptions of the critical components and operational guidelines for the standard hydraulic impulse machine for testing hydraulic hose assemblies, tubing, coils, fittings and similar fluid system components. This revision to the AIR1228 provides a description of a system that meets the requirements for specifications including: AS603, AS4265, and ARP1383. This impulse system utilizes closed loop servo control with specifically generated command signal waveforms. Data accuracy and integrity are emphasized in this revision. Knowing the uncertainty of the pressure measurement is important whether using a resonator tube system, as described in the original release of this document, or a closed-loop systems as described in this release. The accuracy of the data measurement system and consistency of the pressure waveform are fundamental to test validity, regardless of the system type. This is discussed in more detail in Section 5. The standard impulse test system is established for the following purposes: A As referee in the event of conflicting data from two or more nonstandard impulse machines. Such a referee system might be built by an impartial testing activity. B A design guide for future test systems being built by manufacturers and users, or the upgrading of present systems. C A design guide for higher pressure test systems or special purpose machines being designed. It is not the intention of this document to obsolete present resonator type machines. The specification for the resonator type machine is available in the original release of this document. A simple block diagram of the revised system is shown in Figure 1. The simplified block diagram shown in Figure 1 does not use a resonator tube as in the original release of the specification. To eliminate undesired resonances the hydraulic system is as closely coupled as possible. In this design, the pressure waveform is created in closed loop proportional control via the command signal generated by the test controller system. If the test controller is a computer with an impulse specific software application, it is possible to control all parameters of the specified waveform, within the capabilities of the hydraulic system. These parameters include things such as rise rate, damping, secondary oscillation amplitude, etc. In a resonator tube system, it is difficult to make adjustments to these parameters.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This SAE Aerospace Recommended Practice (ARP) is an application guide for fixed and variable displacement hydraulic motors. It provides details of the characteristics of fixed and variable displacement hydraulic motors, architectures, circuit designs, controls, and typical applications. The applications include airborne and defense vehicles with emphasis on high performance applications.
A-6C4 Power Sources Committee
This document applies to special purpose equipment which is used in the ground handling, servicing, and maintenance of transport aircraft. Fixed airport facilities and equipment covered under other sections of Part 1910 of Code of Federal Regulations (OSHA) are excluded from the scope of this document.
AGE-3 Aircraft Ground Support Equipment Committee
This SAE Recommended Practice provides guidance for defining the requirements for evaluating hydraulic pumps and motors and for preparing detailed specifications for these components. The user can follow this document to set forth the pump and motor environmental and performance considerations, establish service life and reliability goals, and define specific evaluation tests for marine vehicle applications.
Ship Fluid Systems Committee
This procedure will be generally applicable to three classes of hydraulic components as listed below:
A-6C1 Fluids and Contamination Control Committee
This SAE Aerospace Recommended Practice (ARP) provides guidance for the design and installation of a commercial aircraft hydraulic system to meet the applicable requirements, including the applicable airworthiness regulations that affect the hydraulic system design. This ARP also provides information and guidelines on the many factors that arise in the design process to provide cost effectiveness, reliability, maintainability and accepted design and installation practices.
A-6A1 Commercial Aircraft Committee
Gas compressors (air and other compressible fluids) have been used sporadically since the 1940's for various utility functions in aerospace applications. They have been used to provide power to gun purge and drive systems, engine or APU starters (recharge accumulators), reservoir pressurization, cockpit pressurization, braking systems, canopy seals, engine control devices, landing gear activation, and boosted flight controls (see Table 1). In current state-of-the-art aircraft, most pneumatic system power is extracted from a stage of compression in the turbo-jet engine. As more and more demands are put on new generation engines for fuel economy and performance there is an increasing need for a new source of pneumatic power. This document is intended to describe current state-of-the-art technology in compressors, define the limitations, discuss enhancements needed and attempt to predict the needs of the future.
A-6C4 Power Sources Committee
Much of the available long-term storage test data has been reviewed and topically separated to enable the independent discussion of storage effects on fluids, seals, hydraulic components, and hydraulic systems. Comments are made in Section 4 concerning the applicability of the test results and regarding design practices for storability. Conclusions are drawn in Section 5 regarding inactive storage of hydraulic systems for at least a 7 year period.
A-6A2 Military Aircraft Committee
Fluid pressure pulsation in a fluid system is an inherent consideration in applications such as aircraft engine and control systems where mechanical component fatigue life and flow performance are critical. Positive displacement pumps transmitting fluid through hydraulic lines under high pressure impart periodic flow pulses to the fluid which can induce undesirable pressure ripple. Some failures of advanced aircraft prototype hardware were traced to a break in the hydraulic component of the control system due to severe localized responses to periodic pressure pulsations produced by a pump flow-induced ripple at the system resonant frequency. This response is associated with a strong structural fluid resonance that is not sufficiently damped by fluid leakage internal to the aircraft hydraulic system. In the case of pumps or hydraulic motors the main source of pulsation energy is in the flow-induced pressure wave associated with the system plumbing pressure pulsations. The pressure wave may propagate in both the pumping wall and fluid as a result of fluid/structure coupling. For a high level of pressure pulsation, the resulting pumping wall motion can then cause mechanical fatigue and unwanted radiated noise and cavitation. This report describes the application of CFD analysis in an aircraft engine control system's vane pumps with a non-intrusive fluid wave in the system. The ultimate goal is to understand the root cause of the pressure pulses and to define improvements or corrective action.
Ni, William W.Bartholme, DanielCass, Michael
Hydraulic systems are used on marine vehicles for steering, vehicle control, and utility services. System components that generate and transmit noise are of concern. This SAE Information Report (a) addresses noise requirements which may apply to the hydraulic systems of ships and submersibles, and (b) identifies noise sources and techniques which may be used to reduce system noise. Noise of power sources (e.g., electric motors) and end items (e.g., steering linkages) is beyond the scope of this document.
Ship Fluid Systems Committee
The marine environment differs greatly from other environments in which hydraulics are used. This Recommended Practice provides hydraulic design considerations and criteria for the marine environment and is applicable to commercial vessels, military ships, and submersible vehicles. This document may be used for manned and un-manned vehicles.
Ship Fluid Systems Committee
This SAE Aerospace Recommended Practice (ARP) covers various requirements for airport runway plows, ramp plows, wings, and hitches to be used with various carrier vehicles primarily used to cast snow away from airport airside operational areas, such as runways, ramps, and taxiways. It does not apply to plows and hitches for non-airport snow removal equipment such as highway plows or construction/farm machinery.
G-15 Airport Snow and Ice Control Equipment Committee
In order to reduce fuel consumption, companies have been looking at hybridizing vehicles. So far, two main hybridization options have been considered: electric and hydraulic hybrids. Because of light duty vehicle operating conditions and the high energy density of batteries, electric hybrids are being widely used for cars. However, companies are still evaluating both hybridization options for medium and heavy duty vehicles. Trucks generally demand very large regenerative power and frequent stop-and-go. In that situation, hydraulic systems could offer an advantage over electric drive systems because the hydraulic motor and accumulator can handle high power with small volume capacity. This study compares the fuel displacement of class 6 trucks using a hydraulic system compared to conventional and hybrid electric vehicles. The paper will describe the component technology and sizes of each powertrain as well as their overall vehicle level control strategies. The fuel consumption will be evaluated on several driving cycles. The paper will then recommend specific powertrain configurations (i.e., hydraulic vs. electric hybrids) depending on specific driving conditions.
Kim, NamwookRousseau, Aymeric
To describe laboratory methods for determining and reporting the contaminant level of the wetted portion of hydraulic fluid power components, parts, subsystems and systems, and of fill fluids. For each type of item it provides a method of obtaining the liquid sample and the contamination level thereof. It also includes procedures for establishing a sampling plan and guidelines for establishing levels of acceptance, but does not set those levels.
CTTC C1, Hydraulic Systems
This SAE Aerospace Information Report (AIR) presents a review of the types and general characteristics of power sources that may be used to provide the power for gaseous or liquid fluidic control systems. Fluidic definitions, terminology, units and symbols are defined in Reference 2.1.1.
A-6A3 Flight Control and Vehicle Management Systems Cmt
This SAE Recommended Practice defines minimum requirements for general characteristics, performance, and durability. It is applicable to remanufactured assemblies (factory rebuild) only. This document applies to master cylinder assemblies and components of current established designs but does not cover fluid level sensors, integral proportioning valves, or those master cylinders used in anti-lock brake or traction control systems. These will be covered by other standards. The general characteristics and test procedure are specified in SAE J1693.
Hydraulic Brake Components Standards Committee
This SAE Standard describes a uniform method to calculate and specify travel performance characteristics of hydraulic excavators, material handlers, knuckle boom log loaders, delimbers, feller bunchers, harvesters, processors, and other knuckle boom material handlers. It establishes definitions and specifies machine conditions for calculations and tests. This document applies to crawler mounted machines such as hydraulic excavators as defined in SAE J/ISO 6165 and ISO 7135, and knuckle boom log loaders as defined in SAE J1209 and SAE J2055. This document also applies to certain forestry equipment defined in SAE J1209 and ISO 6814 that have crawler mountings such as delimbers, feller bunchers, harvesters, and processors. Included in the definition of hydraulic excavators are also front shovel, clamshell, and telescoping boom excavators.
MTC1, Earthmoving Machinery
This Aerospace Standard (AS) presents a system of graphic symbols intended primarily for usage in hydraulic and pneumatic system schematic diagrams for all types of aircraft. It is also considered suitable for marine vehicles and other applications and for ancillary documents where schematics are required. Individual graphic symbols shown herein are also considered suitable for use in conjunction with other types of symbols. This AS is intended to promote industry-wide acceptance and understanding of uniform standards and employs, where possible, symbols which are internationally recognized.
A-6 Aerospace Actuation, Control and Fluid Power Systems
This standard is applicable to off-road work machines - base machine and its equipment included in categories 1.1, 1.2, 2, 4, and 5 of SAE J1116.
MTC1, Earthmoving Machinery
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